Three-dimensional nosetip shape changes in hypersonic flow. I - Illustration of a mathematical model-characteristic method
- 16 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Roughness-induced boundary-layer transition on blunt bodies.AIAA Journal, 1972
- Low temperature ablator nosetip shape change at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Heat-transfer correlations for blunt cones at angle of attackJournal of Spacecraft and Rockets, 1971
- Extension of Emmons' spot theory to flows on blunt bodiesAIAA Journal, 1971
- Methods of Mathematical PhysicsPhysics Today, 1962